Results are presented concerning crack location, cycles to crack initiation, crack propagation, and residual static strength of 18 outer panels of T-29A aircraft; constant amplitude tests were performed by using resonant frequency method at 3 different alternating load levels superimposed on 1 g or level flight mean load.


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    Titel :

    Fatigue investigation of full-scale wing panels of 7075 aluminum alloy


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Castle, C.B. (Autor:in) / Ward, J.F. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    31 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Fatigue Investigation of Full-Scale Wing Panels of 7075 Aluminum Alloy

    Castle, Claude B. / Ward, John F. | NTRS | 1961


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    Aluminum Alloy 7075, Plate and Sheet

    SAE Technical Papers | 2007